CA1090662A - Composite coating of enhanced resistance to attack - Google Patents
Composite coating of enhanced resistance to attackInfo
- Publication number
- CA1090662A CA1090662A CA305,689A CA305689A CA1090662A CA 1090662 A CA1090662 A CA 1090662A CA 305689 A CA305689 A CA 305689A CA 1090662 A CA1090662 A CA 1090662A
- Authority
- CA
- Canada
- Prior art keywords
- undercoating
- chromium
- composition
- coating
- resin
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 238000000576 coating method Methods 0.000 title claims description 28
- 239000011248 coating agent Substances 0.000 title claims description 23
- 239000002131 composite material Substances 0.000 title claims description 10
- 239000000203 mixture Substances 0.000 claims description 43
- 229910052751 metal Inorganic materials 0.000 claims description 31
- 239000002184 metal Substances 0.000 claims description 31
- 239000000758 substrate Substances 0.000 claims description 31
- 239000012948 isocyanate Substances 0.000 claims description 17
- 150000002513 isocyanates Chemical class 0.000 claims description 17
- 238000000034 method Methods 0.000 claims description 15
- 239000000126 substance Substances 0.000 claims description 15
- 239000000049 pigment Substances 0.000 claims description 14
- 229910052804 chromium Inorganic materials 0.000 claims description 11
- 239000011651 chromium Substances 0.000 claims description 11
- 239000008199 coating composition Substances 0.000 claims description 11
- 229920005989 resin Polymers 0.000 claims description 11
- 239000011347 resin Substances 0.000 claims description 11
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 10
- 238000005260 corrosion Methods 0.000 claims description 9
- 230000007797 corrosion Effects 0.000 claims description 9
- 238000001035 drying Methods 0.000 claims description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 9
- 239000003638 chemical reducing agent Substances 0.000 claims description 8
- JOPOVCBBYLSVDA-UHFFFAOYSA-N chromium(6+) Chemical compound [Cr+6] JOPOVCBBYLSVDA-UHFFFAOYSA-N 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 7
- 239000007788 liquid Substances 0.000 claims description 6
- 229920000647 polyepoxide Polymers 0.000 claims description 6
- 239000003822 epoxy resin Substances 0.000 claims description 5
- 125000002887 hydroxy group Chemical group [H]O* 0.000 claims description 5
- 239000004593 Epoxy Substances 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000004132 cross linking Methods 0.000 claims description 3
- 150000002148 esters Chemical class 0.000 claims description 3
- 125000001424 substituent group Chemical group 0.000 claims description 3
- 239000004925 Acrylic resin Substances 0.000 claims description 2
- 229920000178 Acrylic resin Polymers 0.000 claims description 2
- 239000000020 Nitrocellulose Substances 0.000 claims description 2
- 239000011872 intimate mixture Substances 0.000 claims description 2
- 229920001220 nitrocellulos Polymers 0.000 claims description 2
- 229920006122 polyamide resin Polymers 0.000 claims description 2
- 239000011236 particulate material Substances 0.000 claims 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 18
- 239000003973 paint Substances 0.000 description 16
- 239000011701 zinc Substances 0.000 description 14
- 229910052725 zinc Inorganic materials 0.000 description 14
- 238000012360 testing method Methods 0.000 description 13
- 229910052782 aluminium Inorganic materials 0.000 description 12
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 12
- 239000002904 solvent Substances 0.000 description 11
- 238000004140 cleaning Methods 0.000 description 8
- 239000011230 binding agent Substances 0.000 description 7
- 239000003795 chemical substances by application Substances 0.000 description 7
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 7
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 6
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 6
- 239000007921 spray Substances 0.000 description 6
- 239000002966 varnish Substances 0.000 description 6
- 239000002253 acid Substances 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 150000003839 salts Chemical class 0.000 description 4
- KZNICNPSHKQLFF-UHFFFAOYSA-N succinimide Chemical compound O=C1CCC(=O)N1 KZNICNPSHKQLFF-UHFFFAOYSA-N 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- KWYUFKZDYYNOTN-UHFFFAOYSA-M Potassium hydroxide Chemical compound [OH-].[K+] KWYUFKZDYYNOTN-UHFFFAOYSA-M 0.000 description 3
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 3
- 150000007513 acids Chemical class 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- KRVSOGSZCMJSLX-UHFFFAOYSA-L chromic acid Substances O[Cr](O)(=O)=O KRVSOGSZCMJSLX-UHFFFAOYSA-L 0.000 description 3
- 239000000306 component Substances 0.000 description 3
- 239000000470 constituent Substances 0.000 description 3
- 238000009472 formulation Methods 0.000 description 3
- AWJWCTOOIBYHON-UHFFFAOYSA-N furo[3,4-b]pyrazine-5,7-dione Chemical compound C1=CN=C2C(=O)OC(=O)C2=N1 AWJWCTOOIBYHON-UHFFFAOYSA-N 0.000 description 3
- 239000003208 petroleum Substances 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- KDYFGRWQOYBRFD-UHFFFAOYSA-N succinic acid Chemical compound OC(=O)CCC(O)=O KDYFGRWQOYBRFD-UHFFFAOYSA-N 0.000 description 3
- WSFSSNUMVMOOMR-UHFFFAOYSA-N Formaldehyde Chemical compound O=C WSFSSNUMVMOOMR-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N Phenol Chemical compound OC1=CC=CC=C1 ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- DKGAVHZHDRPRBM-UHFFFAOYSA-N Tert-Butanol Chemical compound CC(C)(C)O DKGAVHZHDRPRBM-UHFFFAOYSA-N 0.000 description 2
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 2
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 2
- 229920000180 alkyd Polymers 0.000 description 2
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 description 2
- 150000008280 chlorinated hydrocarbons Chemical class 0.000 description 2
- 238000005238 degreasing Methods 0.000 description 2
- -1 e.g. Substances 0.000 description 2
- 238000005530 etching Methods 0.000 description 2
- 239000004922 lacquer Substances 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 235000019198 oils Nutrition 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 229960002317 succinimide Drugs 0.000 description 2
- VZGDMQKNWNREIO-UHFFFAOYSA-N tetrachloromethane Chemical compound ClC(Cl)(Cl)Cl VZGDMQKNWNREIO-UHFFFAOYSA-N 0.000 description 2
- LWIHDJKSTIGBAC-UHFFFAOYSA-K tripotassium phosphate Chemical compound [K+].[K+].[K+].[O-]P([O-])([O-])=O LWIHDJKSTIGBAC-UHFFFAOYSA-K 0.000 description 2
- 229920002554 vinyl polymer Polymers 0.000 description 2
- 238000011179 visual inspection Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 239000001039 zinc pigment Substances 0.000 description 2
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 1
- RSWGJHLUYNHPMX-UHFFFAOYSA-N Abietic-Saeure Natural products C12CCC(C(C)C)=CC2=CCC2C1(C)CCCC2(C)C(O)=O RSWGJHLUYNHPMX-UHFFFAOYSA-N 0.000 description 1
- HRPVXLWXLXDGHG-UHFFFAOYSA-N Acrylamide Chemical compound NC(=O)C=C HRPVXLWXLXDGHG-UHFFFAOYSA-N 0.000 description 1
- 241000894006 Bacteria Species 0.000 description 1
- 101100021573 Caenorhabditis elegans lon-8 gene Proteins 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 235000008733 Citrus aurantifolia Nutrition 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- CKLJMWTZIZZHCS-REOHCLBHSA-N L-aspartic acid Chemical compound OC(=O)[C@@H](N)CC(O)=O CKLJMWTZIZZHCS-REOHCLBHSA-N 0.000 description 1
- 235000004431 Linum usitatissimum Nutrition 0.000 description 1
- 240000006240 Linum usitatissimum Species 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- CTQNGGLPUBDAKN-UHFFFAOYSA-N O-Xylene Chemical compound CC1=CC=CC=C1C CTQNGGLPUBDAKN-UHFFFAOYSA-N 0.000 description 1
- KHPCPRHQVVSZAH-HUOMCSJISA-N Rosin Natural products O(C/C=C/c1ccccc1)[C@H]1[C@H](O)[C@@H](O)[C@@H](O)[C@@H](CO)O1 KHPCPRHQVVSZAH-HUOMCSJISA-N 0.000 description 1
- 239000004115 Sodium Silicate Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 235000011941 Tilia x europaea Nutrition 0.000 description 1
- XSTXAVWGXDQKEL-UHFFFAOYSA-N Trichloroethylene Chemical compound ClC=C(Cl)Cl XSTXAVWGXDQKEL-UHFFFAOYSA-N 0.000 description 1
- 229920001807 Urea-formaldehyde Polymers 0.000 description 1
- 230000002378 acidificating effect Effects 0.000 description 1
- 229920006397 acrylic thermoplastic Polymers 0.000 description 1
- 238000013019 agitation Methods 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- CEGOLXSVJUTHNZ-UHFFFAOYSA-K aluminium tristearate Chemical compound [Al+3].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O CEGOLXSVJUTHNZ-UHFFFAOYSA-K 0.000 description 1
- 229940063655 aluminum stearate Drugs 0.000 description 1
- 125000003118 aryl group Chemical group 0.000 description 1
- 235000003704 aspartic acid Nutrition 0.000 description 1
- 230000003190 augmentative effect Effects 0.000 description 1
- 238000000498 ball milling Methods 0.000 description 1
- OQFSQFPPLPISGP-UHFFFAOYSA-N beta-carboxyaspartic acid Natural products OC(=O)C(N)C(C(O)=O)C(O)=O OQFSQFPPLPISGP-UHFFFAOYSA-N 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- KDYFGRWQOYBRFD-NUQCWPJISA-N butanedioic acid Chemical compound O[14C](=O)CC[14C](O)=O KDYFGRWQOYBRFD-NUQCWPJISA-N 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 239000000292 calcium oxide Substances 0.000 description 1
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 1
- 125000004432 carbon atom Chemical group C* 0.000 description 1
- 239000004359 castor oil Substances 0.000 description 1
- 235000019438 castor oil Nutrition 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000001913 cellulose Substances 0.000 description 1
- 229920002678 cellulose Polymers 0.000 description 1
- 229920002301 cellulose acetate Polymers 0.000 description 1
- 238000013034 coating degradation Methods 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000000084 colloidal system Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 210000003298 dental enamel Anatomy 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- GUJOJGAPFQRJSV-UHFFFAOYSA-N dialuminum;dioxosilane;oxygen(2-);hydrate Chemical compound O.[O-2].[O-2].[O-2].[Al+3].[Al+3].O=[Si]=O.O=[Si]=O.O=[Si]=O.O=[Si]=O GUJOJGAPFQRJSV-UHFFFAOYSA-N 0.000 description 1
- 150000001991 dicarboxylic acids Chemical class 0.000 description 1
- SOCTUWSJJQCPFX-UHFFFAOYSA-N dichromate(2-) Chemical class [O-][Cr](=O)(=O)O[Cr]([O-])(=O)=O SOCTUWSJJQCPFX-UHFFFAOYSA-N 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 125000003700 epoxy group Chemical group 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 235000004426 flaxseed Nutrition 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- ZEMPKEQAKRGZGQ-XOQCFJPHSA-N glycerol triricinoleate Natural products CCCCCC[C@@H](O)CC=CCCCCCCCC(=O)OC[C@@H](COC(=O)CCCCCCCC=CC[C@@H](O)CCCCCC)OC(=O)CCCCCCCC=CC[C@H](O)CCCCCC ZEMPKEQAKRGZGQ-XOQCFJPHSA-N 0.000 description 1
- 150000002334 glycols Chemical class 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- UCNNJGDEJXIUCC-UHFFFAOYSA-L hydroxy(oxo)iron;iron Chemical compound [Fe].O[Fe]=O.O[Fe]=O UCNNJGDEJXIUCC-UHFFFAOYSA-L 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- SZVJSHCCFOBDDC-UHFFFAOYSA-N iron(II,III) oxide Inorganic materials O=[Fe]O[Fe]O[Fe]=O SZVJSHCCFOBDDC-UHFFFAOYSA-N 0.000 description 1
- 239000004816 latex Substances 0.000 description 1
- 229920000126 latex Polymers 0.000 description 1
- 239000004571 lime Substances 0.000 description 1
- 239000000944 linseed oil Substances 0.000 description 1
- 235000021388 linseed oil Nutrition 0.000 description 1
- 150000002680 magnesium Chemical class 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 150000007522 mineralic acids Chemical class 0.000 description 1
- 229910052901 montmorillonite Inorganic materials 0.000 description 1
- XULSCZPZVQIMFM-IPZQJPLYSA-N odevixibat Chemical compound C12=CC(SC)=C(OCC(=O)N[C@@H](C(=O)N[C@@H](CC)C(O)=O)C=3C=CC(O)=CC=3)C=C2S(=O)(=O)NC(CCCC)(CCCC)CN1C1=CC=CC=C1 XULSCZPZVQIMFM-IPZQJPLYSA-N 0.000 description 1
- 239000005012 oleoresinous Substances 0.000 description 1
- 150000007524 organic acids Chemical class 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000012188 paraffin wax Substances 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 229920003229 poly(methyl methacrylate) Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920001228 polyisocyanate Polymers 0.000 description 1
- 239000005056 polyisocyanate Substances 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000012266 salt solution Substances 0.000 description 1
- 238000005201 scrubbing Methods 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 235000011121 sodium hydroxide Nutrition 0.000 description 1
- 235000019795 sodium metasilicate Nutrition 0.000 description 1
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 1
- 229910052911 sodium silicate Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000001384 succinic acid Substances 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 239000012209 synthetic fiber Substances 0.000 description 1
- ISXSCDLOGDJUNJ-UHFFFAOYSA-N tert-butyl prop-2-enoate Chemical compound CC(C)(C)OC(=O)C=C ISXSCDLOGDJUNJ-UHFFFAOYSA-N 0.000 description 1
- 150000003509 tertiary alcohols Chemical class 0.000 description 1
- ADUQGQSOYWRHCA-UHFFFAOYSA-J tetrasodium;hydroxide;phosphate Chemical compound [OH-].[Na+].[Na+].[Na+].[Na+].[O-]P([O-])([O-])=O ADUQGQSOYWRHCA-UHFFFAOYSA-J 0.000 description 1
- DVKJHBMWWAPEIU-UHFFFAOYSA-N toluene 2,4-diisocyanate Chemical compound CC1=CC=C(N=C=O)C=C1N=C=O DVKJHBMWWAPEIU-UHFFFAOYSA-N 0.000 description 1
- KHPCPRHQVVSZAH-UHFFFAOYSA-N trans-cinnamyl beta-D-glucopyranoside Natural products OC1C(O)C(O)C(CO)OC1OCC=CC1=CC=CC=C1 KHPCPRHQVVSZAH-UHFFFAOYSA-N 0.000 description 1
- 229960002415 trichloroethylene Drugs 0.000 description 1
- UBOXGVDOUJQMTN-UHFFFAOYSA-N trichloroethylene Natural products ClCC(Cl)Cl UBOXGVDOUJQMTN-UHFFFAOYSA-N 0.000 description 1
- 229910000404 tripotassium phosphate Inorganic materials 0.000 description 1
- 235000019798 tripotassium phosphate Nutrition 0.000 description 1
- 239000002383 tung oil Substances 0.000 description 1
- 239000003981 vehicle Substances 0.000 description 1
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- 229920001285 xanthan gum Polymers 0.000 description 1
- 239000000230 xanthan gum Substances 0.000 description 1
- 229940082509 xanthan gum Drugs 0.000 description 1
- 235000010493 xanthan gum Nutrition 0.000 description 1
- 239000008096 xylene Substances 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D7/00—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
- B05D7/14—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials to metal, e.g. car bodies
- B05D7/16—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials to metal, e.g. car bodies using synthetic lacquers or varnishes
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
- C08G18/00—Polymeric products of isocyanates or isothiocyanates
- C08G18/06—Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen
- C08G18/28—Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen characterised by the compounds used containing active hydrogen
- C08G18/40—High-molecular-weight compounds
- C08G18/58—Epoxy resins
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
- C08G18/00—Polymeric products of isocyanates or isothiocyanates
- C08G18/06—Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen
- C08G18/70—Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen characterised by the isocyanates or isothiocyanates used
- C08G18/72—Polyisocyanates or polyisothiocyanates
- C08G18/80—Masked polyisocyanates
- C08G18/8061—Masked polyisocyanates masked with compounds having only one group containing active hydrogen
- C08G18/8064—Masked polyisocyanates masked with compounds having only one group containing active hydrogen with monohydroxy compounds
- C08G18/8067—Masked polyisocyanates masked with compounds having only one group containing active hydrogen with monohydroxy compounds phenolic compounds
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C22/00—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C22/73—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals characterised by the process
- C23C22/74—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals characterised by the process for obtaining burned-in conversion coatings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/10—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by other chemical means
- B05D3/102—Pretreatment of metallic substrates
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D7/00—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
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Abstract
ABSTRACT OF THE DISCLOSURE
Composite coatings, established on metal substrates, now exhibit en-hanced film integrity, such as when exposed to chemicals, solvents and salt.
Additional desirable coating characteristics are also maintained. The undercoating of the composite contains a hexavalent-chromium-providing substance. Included in the topcoating applied over the uncured undercoating is a hydroxyl-containing resin and isocyanate adduct. Subsequent heating fully develops the undercoat curing while concomitantly curing the topcoating.
Composite coatings, established on metal substrates, now exhibit en-hanced film integrity, such as when exposed to chemicals, solvents and salt.
Additional desirable coating characteristics are also maintained. The undercoating of the composite contains a hexavalent-chromium-providing substance. Included in the topcoating applied over the uncured undercoating is a hydroxyl-containing resin and isocyanate adduct. Subsequent heating fully develops the undercoat curing while concomitantly curing the topcoating.
Description
lO~
COMPOSITE COATING OF ENHANCD RESISTANCE TO ATTACK
E~ACKGROUND OF THE INVENTION
Coating compositions for metal substrates that are applied prior to painting, and that contain a hexavalent-chromium-prov~ding substance, may further contain a finely divided metal. For example, in U.S. Patent No. 3,671,331 there are disclosed pulverulent metal containing chromium bonding compositions that contain, in addition to the chromium substance, a reducing agent for sl;ch substance and a particulate metal such as pulverulent zinc. Also, U.S. Patent No. 3,687,739 discloses the preparation of a treated metal surface wherein such treatment includes application of a composition containing, among other constituents but as critical ingredients, chromic acid and a particulate metal.
In composite coating techniques, it has been known to dry an under-coating, which needs curing, and then apply a topcoating. A single curing step then follows to cure both the undercoating and the topcoating as has been disclosed, for example, in British Patent No. 845,259. As has been taught in U.S. Patent No.
4,020,220, applied coatings from compositions that contain a hexavalent-chromium-providing substance which is susceptible to valency reduction to a lower valence state during curing, may also be topcoated and then subsequently be fully cured.
After the precoat application, then the topcoat application, and the final curing, the resulting coated article must usually exhibit a wide variety of desirable characteristics. Exemplary of these are coating adhesion during metal forming operations, plus retention of weldability where the coated substrate would otherwise be weldable. Resistance to attack, and particularly as exhibited against corroslve attack of the metal substrate, is critical. Resistance to other agents, such as acids and solvents, is also often needed.
SUMMARY OF THE INVENTION
It has now been found that a final curing operation will not only fully cure the undercoating but will also, at the same time, cure the topcoating while providing a composite coating havin~ enhanced characteristics. This final cure operation for
COMPOSITE COATING OF ENHANCD RESISTANCE TO ATTACK
E~ACKGROUND OF THE INVENTION
Coating compositions for metal substrates that are applied prior to painting, and that contain a hexavalent-chromium-prov~ding substance, may further contain a finely divided metal. For example, in U.S. Patent No. 3,671,331 there are disclosed pulverulent metal containing chromium bonding compositions that contain, in addition to the chromium substance, a reducing agent for sl;ch substance and a particulate metal such as pulverulent zinc. Also, U.S. Patent No. 3,687,739 discloses the preparation of a treated metal surface wherein such treatment includes application of a composition containing, among other constituents but as critical ingredients, chromic acid and a particulate metal.
In composite coating techniques, it has been known to dry an under-coating, which needs curing, and then apply a topcoating. A single curing step then follows to cure both the undercoating and the topcoating as has been disclosed, for example, in British Patent No. 845,259. As has been taught in U.S. Patent No.
4,020,220, applied coatings from compositions that contain a hexavalent-chromium-providing substance which is susceptible to valency reduction to a lower valence state during curing, may also be topcoated and then subsequently be fully cured.
After the precoat application, then the topcoat application, and the final curing, the resulting coated article must usually exhibit a wide variety of desirable characteristics. Exemplary of these are coating adhesion during metal forming operations, plus retention of weldability where the coated substrate would otherwise be weldable. Resistance to attack, and particularly as exhibited against corroslve attack of the metal substrate, is critical. Resistance to other agents, such as acids and solvents, is also often needed.
SUMMARY OF THE INVENTION
It has now been found that a final curing operation will not only fully cure the undercoating but will also, at the same time, cure the topcoating while providing a composite coating havin~ enhanced characteristics. This final cure operation for
- 2 ~
-- 10~
both the undercoating and the topcoating is referred to herein for convenience as "monobaking." By incorporating isocyanate adduct into the applied topcoating, this monobaking can be effected without variation from the procedure with coatings not containing such adduct.
For the resulting composite coating, the sought after enhan;ement of resistance to chemical attack, such as acid resistance, as well as resistance to solvent attack is achieved. Other, expected coating character-stics are not diminished.
Rather, shear adhesion can be enhanced. Also, the storage life of the topcoat composition is unaltered. Unexpectedly, corrosion resistance for the coated metal substrate such as exhibited in salt spray testing is most desirably augmented.
In one aspect, the present invention is directed to the method of preparing a chemical and corrosion resistant coated metal substrate. The method first com-prises establishing on the surface of the substrate an undercoating containing from about 50 to about 5,000 milligrams per square foot of coated substrate of pulverulent metal in intimate mixture with a substantially resin-free hexavalent-chromium-containing coating composition. Such composition contains a hexavalent-chromium-providing substance and reducing agent therefor in liquid medium. The composition is present in an amount sufficient to provide the coating with from about 5 to about 500 milligrams per square foot of coated substrate of chromium.
The method of the invention next comprises drying the resulting under-coated substrate at a temperature and for a period of time sufficient to vaporize volatile substituents from the coating composition, but insufficient to provide a water-resistant undercoating having substantial orientation of the hexavalent chromium towards reduction. The method next comprises apolying on the dry undercoating a topcoat composition comprising hydroxyl-containing resin, particulate, electrically conductive pigment and less than about 5%, basis total topcoat composition wei~ht, of isocyanate adduct capable of unblocking at a temperature above about 350~.
The method of this aspect of the invention lastly comprises heating the resulting coated article to a temperature above 350F and for a period of time suf-
-- 10~
both the undercoating and the topcoating is referred to herein for convenience as "monobaking." By incorporating isocyanate adduct into the applied topcoating, this monobaking can be effected without variation from the procedure with coatings not containing such adduct.
For the resulting composite coating, the sought after enhan;ement of resistance to chemical attack, such as acid resistance, as well as resistance to solvent attack is achieved. Other, expected coating character-stics are not diminished.
Rather, shear adhesion can be enhanced. Also, the storage life of the topcoat composition is unaltered. Unexpectedly, corrosion resistance for the coated metal substrate such as exhibited in salt spray testing is most desirably augmented.
In one aspect, the present invention is directed to the method of preparing a chemical and corrosion resistant coated metal substrate. The method first com-prises establishing on the surface of the substrate an undercoating containing from about 50 to about 5,000 milligrams per square foot of coated substrate of pulverulent metal in intimate mixture with a substantially resin-free hexavalent-chromium-containing coating composition. Such composition contains a hexavalent-chromium-providing substance and reducing agent therefor in liquid medium. The composition is present in an amount sufficient to provide the coating with from about 5 to about 500 milligrams per square foot of coated substrate of chromium.
The method of the invention next comprises drying the resulting under-coated substrate at a temperature and for a period of time sufficient to vaporize volatile substituents from the coating composition, but insufficient to provide a water-resistant undercoating having substantial orientation of the hexavalent chromium towards reduction. The method next comprises apolying on the dry undercoating a topcoat composition comprising hydroxyl-containing resin, particulate, electrically conductive pigment and less than about 5%, basis total topcoat composition wei~ht, of isocyanate adduct capable of unblocking at a temperature above about 350~.
The method of this aspect of the invention lastly comprises heating the resulting coated article to a temperature above 350F and for a period of time suf-
- 3 -lO~V~
ficient to: (a) orient at least a portion of the undercoating hexavalent chromium toward reduction; commensurate with (b) unblocking the isocyanate adduct and pro-viding cross-linking reaction of resulting isocyanate with topcoat resin.
In another aspect, the invention comprises a composite coated metal substrate including an improved topcoat composition.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
The pre-paint coatings, which may also be termed herein as an "undercoating" or "base coating", can contain a particulate metal such as aluminum, manganese, zinc and magnesium. These particulate metals have been disclosed as useful in bonding coating compositions, containing a hexavalent-chromium-providing substance and reducing agent therefor, in U.S. Patent No. 3,671,331.
Of particular interest for the present invention are such bonding coatings Those that are preferred may contain succinic acid and other dicarboxylic acids of up to 14 carbon atoms as the reducing agents, as has been disclosed in U.S. Patent No.
3,382,081. Such acids with the exception of succinic may be used alone, or theseacids can be used in mixture or in mixture with other organic substances exemplified by aspartic acid, acrylamide or succinimide. Additionally useful combinations that are particularly contemplated are combinations of mono-, tri- or polycarboxylic acids in combination with additional organic substances as has been taught in U.S. Patent No. 3,519,S01. Also of particular interest are the teachings in re8ard to reducing agents, that may be acidic in nature, and have been disclosed in U.S. Patent Nos.
3,535,166 and 3,535,167. Of further particular interest are glycols and glycol-ethers and many representative compounds have been shown in U.S. Patent No. 3,679,493.
Substantially all of the pre-paint undercoatings compositions are simply water based, ostensibly for economy. But for additional or alternative substances, to supply the li~uid medium at least for some of these compositions, there have been taught, as in U.S. Patent No. 3,437,531, blends of chlorinated hydrocarbons and a tertiary alcohol including tertiary butyl alcohol as well as alcohols other than tertiary butyl alcohol. It would appear then in the selection of the li~uid medium that economy is of major importance and thus such medium would most always contain readily commercially available liquids. Chromium is typically present in the hexavalent state by incorporation into the undercoating compositions as chromic acid or dichromate salts or the like. During the curing of the applied coating composition, the metal is susceptible to valency reduction to a lower valence state. Such reduction is generally enhanced by the presence of the reducing agent in the composition.
When the undercoating is established, typically by application directly to the surface of the substrate to be coated, although such substrate might be a precoated metal substrate, such as for example, a phosphatized metal substrate, the applied coating will be non-water resistant. That is, such applied coating, prior to curing, can be easily removed by rubbing with a damp cloth.
Although it will reach the condition of a dry coating by any convential drying means, the drying is typically forced drying at elevated temperature. In general, the drying conditions are temperatures below 550~ air temperature, and at such temperature, for times of less than about 2 minutes. However, lower tempera-tures such as 4S0-500F, with drying times, such as 0.5-1.5 minutes are more typically used. The resulting undercoated article may then be cooled before topcoating.
The resulting weight of the undercoating on the metal substrate may vary to a considerable degree, but will most typically always be present in an amountsupplying between about 5-500 milligrams per square foot of chromium, expressed as chromium and not CrO3. Also, the coated metal substrate should contain between about 50 and about 5,000 milligrams per square foot of pulverulent metal and preferably have a weight ratio of chromium to pulverulent metal of not substantially above about 0.3:1.
The undercoating is topcoated with a weldable primer containing an electrically conductive pigment in a vehicle. Nlore particularly, the welding primers are coating compositions containing a particulate, electrically conductive pigment of aluminum, copper, cadmium, steel, carbon, zinc, or magnetite, i.e., the magneticoxide of iron, and including mixtures thereof such as of aluminum flake and zinc '' "- 10~
powder. Generally, the carbon pigments, e.g., channel blacks or furnace blacks, are the most f inely divided of these electrically conductive pigments, often havingparticle size of 0.01 micron for the intensely black pigments. Comparatively, the finely divided aluminum powders have flake thicknesses for the finest grades of about 0.25 micron. These aluminum pigments can be typically produced by stamping, , generally of small pieces of aluminum foil, or by ball milling atomized aluminum formed by air blasting a molten aluminum spray. Typically a finely divided zinc pigment is a distilled zinc dust or particles prepared by atomizing molten zinc in an air stream. Particle size for distilled zinc powders often average from about 2 to la about 6 microns with generally about 99 weight percent or better passing a 240 mesh ~
U.S. Standard Sieve.
Since these primers generally are applied preparatory to subsequent welding of the substrate, they must contain a substantial amount of the electrically conductive pigment, e.g., at least about 30 volume percent pigment for the zinc-rich primers and often more than about 65 percent by volume of particulate pigment, but $ on a weight basis, because of the density of the zinc, these primers can contain up to about 98 weight percent of such pigment.
In formulating the weldable primers, the binder component can be made ` up of resins at least one of which will be hydroxyl-containing. Thus the binder com-ponents for the zinc-rich primer can be polyamide resins combined with epoxy resins, although other binder materials have been found to be compatible with particulate zinc pigment, e.g., acrylic resin, nitrocellulose resin, and epoxy esters including epoxy ester medium oil content linseed oil. It is preferred that the binder component contain some epoxy resin.
~ As a critical constituent the topcoat composition will also contain up to s~ about 5%, basis total topcoat composition weight, of isocyanate adduct. Greater than about 5 weight percent of such adduct is regarded as uneconomical as such greater amount will not provide any commensurate additional benefit. It is possible that as little as 0.01 weight percent of the isocyanate adduct may be present but it is preferable, for efficiency and economy, that the coating composition contain above ~ - 6 -f -` lOS~ Z
i about 0.2 weight percent of the adduct. The adduct should "unblock," i.e., provide reactive isocyanate, at a temperature below 350F. It is typical though for the adduct to provide free isocyanate at a temperature of about lS0C, as has been ~:, discussed, for example, in U.S. Patent No. 2,99S,S31. This allows the blocked isocyanate to be blended in the topcoat composition for subsequent storage, before use.
It is contemplated to use any blocked isocyanate, and for a variety of such, reference can be made to U.S. Patent No. 3,723,372. It is preferred, however, for economy to use a readily commercially available blocked isocyanate and such ¦, 1~ include those formed from toluene 2,4-diisocyanate, or apparent derivatives thereof, which are "blocked" with phenol.
Additionally the topcoating formulations can contain flow control agents, as for example urea formaldehyde resins, thixotroping agents such as silica and organic derivatives of magnesium montmorillonite, and antisettling agents par-ticularly for the aluminum and zinc primers which agents include hydrogenated castor oil and aluminum stearate. Also for the aluminum and zinc primers where gassing can be a problem a gas inhibiting substance such as lime or calcium oxide is generally in-cluded in the formulation. Also, these primers usually contain, and/or are typically cut back after formulation but before application with, petroleum derived hydro-,~ 20 carbon liquids such as toluene, benzene, xylene, and synthetically prepared aromatic ,~ solvent blends from petroleum. Zinc-rich weldable primers have been more extensively reviewed in an article entitled "Zinc-Rich Paints" in Paint and Varnish Production, April, 1964, p. 35 f.: May, '64 p. 87 f.; and June, '64, p. 47 f.
s The final make up of the primer can be dependent upon the method of application of the primer to the treated metal substrate. Typically for primers .~ containing zinc dust or combinations of zinc dust with aluminum flake, or zinc flake ~; with aluminum flake and the like, where such primers are spray applied to the metal substrate they may contain between about 50-80 weight percent of the pulverulentmetal and between about 10-30 weight percent of binder. Also such primers generally are formulated with a few weight percent or less of a thixotroping a~ent, and often J -l'~)~t~
with a half weight percent or less of a metallic drier, e.g., a lead, man~anese, cobalt or other metallic salt of organic acid, and typically 10-30 weight percent of petroleum derived hydrocarbon liquid.
The heating, i.e., the monobaking, of the coating composite can be merely baking in a simple convection oven, as opposed to infrared bakin8. This heating will be at an air temperature above about 350F and at such temperature will usually continue for a time of about 0.S minute and usually a time no longer than about 10 minutes. On the other hand, air temperatures above about 1,000F can be inefficient and lead to film degradation during heating. Typically, the air temperature will be maintained within the range of between about 400-700F with cure times ranging from as quickly at about 2 to 3 minutes up to as lon8 as 10 to 20 minutes.
Before application of the pre-paint coating composition to a metal sub-strate, it is generally advisable to remove foreign matter from the metal surface by thoroughly cleaning and degreasing. Degreasing can be accomplished with known agents such as sodium metasilicate, caustic soda, carbon tetrachloride, trichloroethy-lene and the like. The use of commercial alkaline cleaning compositions can be employed with combine washing and mild abrasive treatment, e.g., an aqueous trisodium phosphate-sodium hydroxide cleaning solution. In addition to cleaning, the substrate can undergo cleaning plus etching, for example, with a strong inorganic acid etching agent.
After coating by the methods of the present invention, the resulting coated substrate can be further topcoated with any suitable paint, i.e., a paint, primer, enamel, varnish, or lacquer. Such paints may contain pigment in a binder or can be unpigmented, e.g., generally cellulose lacquers, rosin varnishes, and oleo-resinous varnishes, as for example tung oil varnish. The paints can be solvent reduced or they may be water reduced, e.g., latex or water-soluble resins, including modified : , or soluble alkyds, or the paints can have reactive solvents such as in the polyesters or polyurethanes. Additional suitable paints which can be used include oil paints, including phenolic resin paints, solvent-reduced alkyds, epoxys, acrylics, vinyl, in-5 30 cluding polyvinyl butryal and oil-~,vax-type coatings such as linseed oil-paraffin wax ~,~
~ .,.
~i t,"i~
i; 10S0f~62 ;
paints. The paints may be applied as mill finishes.
The following example shows a way in which the invention has been prac-ticed but should not be construed as limiting the invention. In the example5 the~ following procedures have been employed.
,~ PREPARATION OF TEST PANELS
Unless otherwise specifically described, test panels are typically 4" x 8"
cold rolled, low carbon steel panels. They are prepared for coating by first scrubbing 1 with a cleaning pad which is a porous, fibrous pad of synthetic fiber impregnated with i ~ an abrasive. Thereafter, the scrubbed panels are immersed in a cleaning solution typically containing chlorinated hydrocarbon and maintained at about 180F., or ~ l containing 1-5 ounces, per gallon of water, of a mixture of 25 weight percent L ~ tripotassium phosphate and 75 weight percent potassium hydroxide. This alkaline bath is maintained at a temperature of about 150- 180F. Following the cleaning, the panels are rinsed with warm water and preferably dried.
SOLVENT RESISTANCE TEST
Painted panels are immersed for sixteen hours in organic solvent. Panels are removed from the solvent and are immediately manually rubbed across the panel j about twenty strokes with a paper tissue while using moderate pressure. Rubbed panels are then visually inspected to see if the undercoating has been exposed during the rubbing, with the film being regarded as soluble if the undercoating has been exposed. Solvents used include benzene, toluene and cellulose acetate.
COE~ROSION RESISTANCE TEST (ASTM E~-117~
Corrosion resistance of coated parts is measured ~y means of the standard v~ ~ salt spray (fog) test for paints and varnishes ASTM ~-117. In this test, the parts are ;i-~ placed in a chamber kept at constant temperature where they are exposed to a fine spray (fog) of a 5% salt solution for specified periods of time, rinsed in water and dried. The extent of corrosion on the test parts is determined by comparing parts one ~, ~ with another, and all by visual inspection. The efficacy of the corrosion resistance ,, ~ g_ ~,... . .
1090~2 obtained on coated panels is, in part, quantitatively evaluated on a numerical scale !' from 0 to 10- The panels are visually inspected and compared with one another and the system is used for convenience in the reviewing of results. In the rating system the following numbers are used to cover the following results:
(0) retention of film integrity, no red rust;
(2) initial coating degradation, pinpoints of red rust;
ficient to: (a) orient at least a portion of the undercoating hexavalent chromium toward reduction; commensurate with (b) unblocking the isocyanate adduct and pro-viding cross-linking reaction of resulting isocyanate with topcoat resin.
In another aspect, the invention comprises a composite coated metal substrate including an improved topcoat composition.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
The pre-paint coatings, which may also be termed herein as an "undercoating" or "base coating", can contain a particulate metal such as aluminum, manganese, zinc and magnesium. These particulate metals have been disclosed as useful in bonding coating compositions, containing a hexavalent-chromium-providing substance and reducing agent therefor, in U.S. Patent No. 3,671,331.
Of particular interest for the present invention are such bonding coatings Those that are preferred may contain succinic acid and other dicarboxylic acids of up to 14 carbon atoms as the reducing agents, as has been disclosed in U.S. Patent No.
3,382,081. Such acids with the exception of succinic may be used alone, or theseacids can be used in mixture or in mixture with other organic substances exemplified by aspartic acid, acrylamide or succinimide. Additionally useful combinations that are particularly contemplated are combinations of mono-, tri- or polycarboxylic acids in combination with additional organic substances as has been taught in U.S. Patent No. 3,519,S01. Also of particular interest are the teachings in re8ard to reducing agents, that may be acidic in nature, and have been disclosed in U.S. Patent Nos.
3,535,166 and 3,535,167. Of further particular interest are glycols and glycol-ethers and many representative compounds have been shown in U.S. Patent No. 3,679,493.
Substantially all of the pre-paint undercoatings compositions are simply water based, ostensibly for economy. But for additional or alternative substances, to supply the li~uid medium at least for some of these compositions, there have been taught, as in U.S. Patent No. 3,437,531, blends of chlorinated hydrocarbons and a tertiary alcohol including tertiary butyl alcohol as well as alcohols other than tertiary butyl alcohol. It would appear then in the selection of the li~uid medium that economy is of major importance and thus such medium would most always contain readily commercially available liquids. Chromium is typically present in the hexavalent state by incorporation into the undercoating compositions as chromic acid or dichromate salts or the like. During the curing of the applied coating composition, the metal is susceptible to valency reduction to a lower valence state. Such reduction is generally enhanced by the presence of the reducing agent in the composition.
When the undercoating is established, typically by application directly to the surface of the substrate to be coated, although such substrate might be a precoated metal substrate, such as for example, a phosphatized metal substrate, the applied coating will be non-water resistant. That is, such applied coating, prior to curing, can be easily removed by rubbing with a damp cloth.
Although it will reach the condition of a dry coating by any convential drying means, the drying is typically forced drying at elevated temperature. In general, the drying conditions are temperatures below 550~ air temperature, and at such temperature, for times of less than about 2 minutes. However, lower tempera-tures such as 4S0-500F, with drying times, such as 0.5-1.5 minutes are more typically used. The resulting undercoated article may then be cooled before topcoating.
The resulting weight of the undercoating on the metal substrate may vary to a considerable degree, but will most typically always be present in an amountsupplying between about 5-500 milligrams per square foot of chromium, expressed as chromium and not CrO3. Also, the coated metal substrate should contain between about 50 and about 5,000 milligrams per square foot of pulverulent metal and preferably have a weight ratio of chromium to pulverulent metal of not substantially above about 0.3:1.
The undercoating is topcoated with a weldable primer containing an electrically conductive pigment in a vehicle. Nlore particularly, the welding primers are coating compositions containing a particulate, electrically conductive pigment of aluminum, copper, cadmium, steel, carbon, zinc, or magnetite, i.e., the magneticoxide of iron, and including mixtures thereof such as of aluminum flake and zinc '' "- 10~
powder. Generally, the carbon pigments, e.g., channel blacks or furnace blacks, are the most f inely divided of these electrically conductive pigments, often havingparticle size of 0.01 micron for the intensely black pigments. Comparatively, the finely divided aluminum powders have flake thicknesses for the finest grades of about 0.25 micron. These aluminum pigments can be typically produced by stamping, , generally of small pieces of aluminum foil, or by ball milling atomized aluminum formed by air blasting a molten aluminum spray. Typically a finely divided zinc pigment is a distilled zinc dust or particles prepared by atomizing molten zinc in an air stream. Particle size for distilled zinc powders often average from about 2 to la about 6 microns with generally about 99 weight percent or better passing a 240 mesh ~
U.S. Standard Sieve.
Since these primers generally are applied preparatory to subsequent welding of the substrate, they must contain a substantial amount of the electrically conductive pigment, e.g., at least about 30 volume percent pigment for the zinc-rich primers and often more than about 65 percent by volume of particulate pigment, but $ on a weight basis, because of the density of the zinc, these primers can contain up to about 98 weight percent of such pigment.
In formulating the weldable primers, the binder component can be made ` up of resins at least one of which will be hydroxyl-containing. Thus the binder com-ponents for the zinc-rich primer can be polyamide resins combined with epoxy resins, although other binder materials have been found to be compatible with particulate zinc pigment, e.g., acrylic resin, nitrocellulose resin, and epoxy esters including epoxy ester medium oil content linseed oil. It is preferred that the binder component contain some epoxy resin.
~ As a critical constituent the topcoat composition will also contain up to s~ about 5%, basis total topcoat composition weight, of isocyanate adduct. Greater than about 5 weight percent of such adduct is regarded as uneconomical as such greater amount will not provide any commensurate additional benefit. It is possible that as little as 0.01 weight percent of the isocyanate adduct may be present but it is preferable, for efficiency and economy, that the coating composition contain above ~ - 6 -f -` lOS~ Z
i about 0.2 weight percent of the adduct. The adduct should "unblock," i.e., provide reactive isocyanate, at a temperature below 350F. It is typical though for the adduct to provide free isocyanate at a temperature of about lS0C, as has been ~:, discussed, for example, in U.S. Patent No. 2,99S,S31. This allows the blocked isocyanate to be blended in the topcoat composition for subsequent storage, before use.
It is contemplated to use any blocked isocyanate, and for a variety of such, reference can be made to U.S. Patent No. 3,723,372. It is preferred, however, for economy to use a readily commercially available blocked isocyanate and such ¦, 1~ include those formed from toluene 2,4-diisocyanate, or apparent derivatives thereof, which are "blocked" with phenol.
Additionally the topcoating formulations can contain flow control agents, as for example urea formaldehyde resins, thixotroping agents such as silica and organic derivatives of magnesium montmorillonite, and antisettling agents par-ticularly for the aluminum and zinc primers which agents include hydrogenated castor oil and aluminum stearate. Also for the aluminum and zinc primers where gassing can be a problem a gas inhibiting substance such as lime or calcium oxide is generally in-cluded in the formulation. Also, these primers usually contain, and/or are typically cut back after formulation but before application with, petroleum derived hydro-,~ 20 carbon liquids such as toluene, benzene, xylene, and synthetically prepared aromatic ,~ solvent blends from petroleum. Zinc-rich weldable primers have been more extensively reviewed in an article entitled "Zinc-Rich Paints" in Paint and Varnish Production, April, 1964, p. 35 f.: May, '64 p. 87 f.; and June, '64, p. 47 f.
s The final make up of the primer can be dependent upon the method of application of the primer to the treated metal substrate. Typically for primers .~ containing zinc dust or combinations of zinc dust with aluminum flake, or zinc flake ~; with aluminum flake and the like, where such primers are spray applied to the metal substrate they may contain between about 50-80 weight percent of the pulverulentmetal and between about 10-30 weight percent of binder. Also such primers generally are formulated with a few weight percent or less of a thixotroping a~ent, and often J -l'~)~t~
with a half weight percent or less of a metallic drier, e.g., a lead, man~anese, cobalt or other metallic salt of organic acid, and typically 10-30 weight percent of petroleum derived hydrocarbon liquid.
The heating, i.e., the monobaking, of the coating composite can be merely baking in a simple convection oven, as opposed to infrared bakin8. This heating will be at an air temperature above about 350F and at such temperature will usually continue for a time of about 0.S minute and usually a time no longer than about 10 minutes. On the other hand, air temperatures above about 1,000F can be inefficient and lead to film degradation during heating. Typically, the air temperature will be maintained within the range of between about 400-700F with cure times ranging from as quickly at about 2 to 3 minutes up to as lon8 as 10 to 20 minutes.
Before application of the pre-paint coating composition to a metal sub-strate, it is generally advisable to remove foreign matter from the metal surface by thoroughly cleaning and degreasing. Degreasing can be accomplished with known agents such as sodium metasilicate, caustic soda, carbon tetrachloride, trichloroethy-lene and the like. The use of commercial alkaline cleaning compositions can be employed with combine washing and mild abrasive treatment, e.g., an aqueous trisodium phosphate-sodium hydroxide cleaning solution. In addition to cleaning, the substrate can undergo cleaning plus etching, for example, with a strong inorganic acid etching agent.
After coating by the methods of the present invention, the resulting coated substrate can be further topcoated with any suitable paint, i.e., a paint, primer, enamel, varnish, or lacquer. Such paints may contain pigment in a binder or can be unpigmented, e.g., generally cellulose lacquers, rosin varnishes, and oleo-resinous varnishes, as for example tung oil varnish. The paints can be solvent reduced or they may be water reduced, e.g., latex or water-soluble resins, including modified : , or soluble alkyds, or the paints can have reactive solvents such as in the polyesters or polyurethanes. Additional suitable paints which can be used include oil paints, including phenolic resin paints, solvent-reduced alkyds, epoxys, acrylics, vinyl, in-5 30 cluding polyvinyl butryal and oil-~,vax-type coatings such as linseed oil-paraffin wax ~,~
~ .,.
~i t,"i~
i; 10S0f~62 ;
paints. The paints may be applied as mill finishes.
The following example shows a way in which the invention has been prac-ticed but should not be construed as limiting the invention. In the example5 the~ following procedures have been employed.
,~ PREPARATION OF TEST PANELS
Unless otherwise specifically described, test panels are typically 4" x 8"
cold rolled, low carbon steel panels. They are prepared for coating by first scrubbing 1 with a cleaning pad which is a porous, fibrous pad of synthetic fiber impregnated with i ~ an abrasive. Thereafter, the scrubbed panels are immersed in a cleaning solution typically containing chlorinated hydrocarbon and maintained at about 180F., or ~ l containing 1-5 ounces, per gallon of water, of a mixture of 25 weight percent L ~ tripotassium phosphate and 75 weight percent potassium hydroxide. This alkaline bath is maintained at a temperature of about 150- 180F. Following the cleaning, the panels are rinsed with warm water and preferably dried.
SOLVENT RESISTANCE TEST
Painted panels are immersed for sixteen hours in organic solvent. Panels are removed from the solvent and are immediately manually rubbed across the panel j about twenty strokes with a paper tissue while using moderate pressure. Rubbed panels are then visually inspected to see if the undercoating has been exposed during the rubbing, with the film being regarded as soluble if the undercoating has been exposed. Solvents used include benzene, toluene and cellulose acetate.
COE~ROSION RESISTANCE TEST (ASTM E~-117~
Corrosion resistance of coated parts is measured ~y means of the standard v~ ~ salt spray (fog) test for paints and varnishes ASTM ~-117. In this test, the parts are ;i-~ placed in a chamber kept at constant temperature where they are exposed to a fine spray (fog) of a 5% salt solution for specified periods of time, rinsed in water and dried. The extent of corrosion on the test parts is determined by comparing parts one ~, ~ with another, and all by visual inspection. The efficacy of the corrosion resistance ,, ~ g_ ~,... . .
1090~2 obtained on coated panels is, in part, quantitatively evaluated on a numerical scale !' from 0 to 10- The panels are visually inspected and compared with one another and the system is used for convenience in the reviewing of results. In the rating system the following numbers are used to cover the following results:
(0) retention of film integrity, no red rust;
(2) initial coating degradation, pinpoints of red rust;
(4) less than 3% red rust basis total surface area of the part;
(6) 3 to 10% red rust, i.e., a significant amount of rust;
(8) 10 to 25 percent surface area red rust;
(10) greater than 2S percent red rust.
EXAMPLE `~
There is formulated, with blending, an undercoating composition con-taining 20 grams per liter of chromic acid, 3.3 grams per liter of succinic acid, 1.7 grams per liter of succinimide, 1.5 grams per liter of xanthan gum hydrophillic colloid, which is a heteropolysccharide prepared from the bacteria specie Xantha-monas camperstris and has a molecular weight in excess of 200,000. Additionally,the composition contains 1 milliliter of formalin, 7 grams per liter of zinc oxide, 120 grams per liter of zinc dust having an average particle size of about 5 microns and having all particles finer than 16 microns, and 1 drop per liter of a wetter which is a nonionic, modified polyethoxide adduct having a viscosity in centipoises at 25C of 180 and a density at 25C of 8.7 lbs. per gallon. After mixing all of these constituents, this undercoating composition is then ready for coating test panels.
Panels, prepared as described hereinabove, are dip coated in the under-coating composition. They are then removed from the composition and excess composition is drained from the panels. Some panels are then baked for 1.5 minutes, and are thereby the "monobal<e" panels, and some for 4 minutes, which are "dibake"
panels9 all in an oven at an oven temperature of 500F.
Panels are then primer topcoated. The primer used is a commercially available primer which is a zinc-rich weldable primer having a weight per gallon of ~ lO~Uf~
about lS.2 Ibs., a solids volume of about 29%, and containing about 64 weight percent solids content. The binder cornponent is prepared from a high molecular weight epoxy resin. The primer has a typical viscosity of about 80 seconds as measured on a No. 4 Ford cup. Prior to use, there is blended, with vigorous agitation, into one batch of ~; the primer O.S weight percen~, basis total batch weight, of a phenol blocked polyisocyanate adduct. The adduct is a yellowish solid having a weight per gallon of 10.6 pounds, an average equivalent weight of 336 and a percentage of available NCO
of ll.S-13.S. Each respective batch of primer is applied to undercoated panels by drawing the primer down over the panel with a No. 18 draw bar to provide a smooth, uniform primer coat, generally of about O.S mil. thickness. Resulting coated panels are cured for either 2-~, or 3, or 4-3~ minutes in an oven at S00F.
In the manner as described hereinabove, panels that have been subjected to the above-described corrosion resistance (salt spray) test are quantitativelyevaluated for corrosion by visual inspection, comparing panels with one another and employing the above-discussed rating system. From the resulting ratings, the results for percentage changes are determined by straight-forward calculation. These results are shown in the table below. Also shown in the table below are results for panels subjected to the above-discussed solvent resistance test.
TABLE
Corrosion Resistance Undercoating Improvement , %:
Cure Time,Min. Solvent Resistance Monobake vs. Dibake Monobake Dibake No Adduct With Adduct No Adduct With Adduct I.S 4 Soluble Insoluble330 Test Hours 100% 120%
520 Test Hours % 130%
(6) 3 to 10% red rust, i.e., a significant amount of rust;
(8) 10 to 25 percent surface area red rust;
(10) greater than 2S percent red rust.
EXAMPLE `~
There is formulated, with blending, an undercoating composition con-taining 20 grams per liter of chromic acid, 3.3 grams per liter of succinic acid, 1.7 grams per liter of succinimide, 1.5 grams per liter of xanthan gum hydrophillic colloid, which is a heteropolysccharide prepared from the bacteria specie Xantha-monas camperstris and has a molecular weight in excess of 200,000. Additionally,the composition contains 1 milliliter of formalin, 7 grams per liter of zinc oxide, 120 grams per liter of zinc dust having an average particle size of about 5 microns and having all particles finer than 16 microns, and 1 drop per liter of a wetter which is a nonionic, modified polyethoxide adduct having a viscosity in centipoises at 25C of 180 and a density at 25C of 8.7 lbs. per gallon. After mixing all of these constituents, this undercoating composition is then ready for coating test panels.
Panels, prepared as described hereinabove, are dip coated in the under-coating composition. They are then removed from the composition and excess composition is drained from the panels. Some panels are then baked for 1.5 minutes, and are thereby the "monobal<e" panels, and some for 4 minutes, which are "dibake"
panels9 all in an oven at an oven temperature of 500F.
Panels are then primer topcoated. The primer used is a commercially available primer which is a zinc-rich weldable primer having a weight per gallon of ~ lO~Uf~
about lS.2 Ibs., a solids volume of about 29%, and containing about 64 weight percent solids content. The binder cornponent is prepared from a high molecular weight epoxy resin. The primer has a typical viscosity of about 80 seconds as measured on a No. 4 Ford cup. Prior to use, there is blended, with vigorous agitation, into one batch of ~; the primer O.S weight percen~, basis total batch weight, of a phenol blocked polyisocyanate adduct. The adduct is a yellowish solid having a weight per gallon of 10.6 pounds, an average equivalent weight of 336 and a percentage of available NCO
of ll.S-13.S. Each respective batch of primer is applied to undercoated panels by drawing the primer down over the panel with a No. 18 draw bar to provide a smooth, uniform primer coat, generally of about O.S mil. thickness. Resulting coated panels are cured for either 2-~, or 3, or 4-3~ minutes in an oven at S00F.
In the manner as described hereinabove, panels that have been subjected to the above-described corrosion resistance (salt spray) test are quantitativelyevaluated for corrosion by visual inspection, comparing panels with one another and employing the above-discussed rating system. From the resulting ratings, the results for percentage changes are determined by straight-forward calculation. These results are shown in the table below. Also shown in the table below are results for panels subjected to the above-discussed solvent resistance test.
TABLE
Corrosion Resistance Undercoating Improvement , %:
Cure Time,Min. Solvent Resistance Monobake vs. Dibake Monobake Dibake No Adduct With Adduct No Adduct With Adduct I.S 4 Soluble Insoluble330 Test Hours 100% 120%
520 Test Hours % 130%
Claims (6)
1. The method of preparing a chemical and corrosion resistant coated metal substrate which method comprises:
(1) establishing on the surface of said substrate an undercoating containing from about 50 to about 5,000 milligrams per square foot of coated substrate of pulverulent metal in intimate mixture with a substantially resin-free hexavalent chromium-containing coating composition con-taining a hexavalent-chromium-providing substance and reducing agent therefor in liquid medium, said composition being present in an amount sufficient to provide said coating with from about 5 to about 500 milligrams per square foot of coated substrate of chromium;
(2) drying the resulting undercoated substrate at a temperature and for a period of time sufficient to vaporize volatile substituents from said coating composition, but insufficient to provide a water-resistant under-coating having substantial orientation of the hexavalent chromium towards reduction;
(3) applying on the dry undercoating a topcoat composition comprising hydroxyl-containing resin, particulate, electrically conductive pigment, and less than about 5%, basis total topcoat composition weight, of isocyanate adduct capable of unlocking at a temperature above about 350°F.; and (4) heating the resulting coated article at a temperature above 350°F. and for a period of time sufficient to: (a) orient at least a portion of the undercoating hexavalent chromium toward reduction; commensurate with, (b) unblocking the isocyanate adduct and providing cross-linking reaction of resulting isocyanate with topcoat resin.
(1) establishing on the surface of said substrate an undercoating containing from about 50 to about 5,000 milligrams per square foot of coated substrate of pulverulent metal in intimate mixture with a substantially resin-free hexavalent chromium-containing coating composition con-taining a hexavalent-chromium-providing substance and reducing agent therefor in liquid medium, said composition being present in an amount sufficient to provide said coating with from about 5 to about 500 milligrams per square foot of coated substrate of chromium;
(2) drying the resulting undercoated substrate at a temperature and for a period of time sufficient to vaporize volatile substituents from said coating composition, but insufficient to provide a water-resistant under-coating having substantial orientation of the hexavalent chromium towards reduction;
(3) applying on the dry undercoating a topcoat composition comprising hydroxyl-containing resin, particulate, electrically conductive pigment, and less than about 5%, basis total topcoat composition weight, of isocyanate adduct capable of unlocking at a temperature above about 350°F.; and (4) heating the resulting coated article at a temperature above 350°F. and for a period of time sufficient to: (a) orient at least a portion of the undercoating hexavalent chromium toward reduction; commensurate with, (b) unblocking the isocyanate adduct and providing cross-linking reaction of resulting isocyanate with topcoat resin.
2. The method of claim 1 wherein the drying of the undercoated substrate is forced drying providing a peak metal temperature not substantially above about 300°F. and the undercoating is cooled prior to application of the topcoat composition.
3. The method of claim 1 wherein the heating at a temperature above 350°F. provides a peak metal temperature above about 400°F.
4. The method of claim 1 wherein the topcoat composition is applied to provide a dry film thickness of between about 0.1-10 mils and said composition contains between about 5-50 percent of hydroxyl-containing resin selected from the group consisting of epoxy resin, polyamide resin combined with epoxy resin, epoxy esters, acrylic resin and nitrocellulose resin.
5. A coated metal substrate protected with a coating composite, wherein a portion of said coating composite comprises an undercoating and a topcoating each containing particulate material and each established from heat curable compositions, with the undercoating also containing, in liquid medium, a hexavalent-chromium-providing substance which is susceptible to valency reduction to a lower valence state during curing of applied composition, said chromium being at least partially present in said composition in the hexavalent higher valency state, said undercoating composi-tion further containing reducing agent for said chromium and having pulverulent metal as said particulate material and with the undercoating being first established in said composite in non water-resistant condition and then dried at a temperature and for a period of time sufficent to vaporize volatile substituents from applied composition but insufficient to orient the undercoating towards reduction of said chromium in said higher valency state, and with said topcoating being applied on the dry undercoating, said topcoating comprising hydroxyl-containing resin, particulate, electrically conductive pigment, and less than about 5%, basis total topcoat composition weight, of isocyanate adduct capable of unblocking at a temperature above about 350°., and wherein the curing after topcoat application is heating at a temperature above 350°F. and for a period of time sufficient to: (a) orient at least a portion of the undercoating hexavalent chromium towards reduction; commensurate with, (b) unblocking the isocyanate adduct and providing cross-linking reaction of resulting isocyanate with topcoat resin.
6. The coated substrate of claim 5 characterized by having said under-coating as the first coating on the surface of said substrate.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/807,785 US4098620A (en) | 1977-06-20 | 1977-06-20 | Composite coating of enhanced resistance to attack |
| US807,785 | 1977-06-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1090662A true CA1090662A (en) | 1980-12-02 |
Family
ID=25197172
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA305,689A Expired CA1090662A (en) | 1977-06-20 | 1978-06-19 | Composite coating of enhanced resistance to attack |
Country Status (14)
| Country | Link |
|---|---|
| US (1) | US4098620A (en) |
| JP (1) | JPS593230B2 (en) |
| AU (1) | AU516375B2 (en) |
| BE (1) | BE868232A (en) |
| BR (1) | BR7803900A (en) |
| CA (1) | CA1090662A (en) |
| DE (1) | DE2826827C2 (en) |
| ES (1) | ES470919A1 (en) |
| FR (1) | FR2395298A1 (en) |
| GB (1) | GB2000050B (en) |
| IT (1) | IT1105548B (en) |
| MX (1) | MX148122A (en) |
| NL (1) | NL182577C (en) |
| SE (1) | SE444001B (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3531370A1 (en) * | 1985-09-03 | 1987-03-05 | Iris Lacke Baumann Gmbh | Paint system for a corrosion-resistant and impact-resistant finish |
| JP2671006B2 (en) * | 1988-04-14 | 1997-10-29 | 日本カーバイド工業株式会社 | Resin composition for top coating of cured coating |
| JPH0735587B2 (en) * | 1988-06-30 | 1995-04-19 | 日本鋼管株式会社 | Manufacturing method of high corrosion resistant surface treated steel sheet |
| JP2770864B2 (en) * | 1990-07-06 | 1998-07-02 | 日本パーカライジング株式会社 | Chromate treatment liquid |
| DE4111701A1 (en) * | 1991-04-10 | 1992-10-15 | Itw Befestigungssysteme | METHOD FOR COATING CORROSION PROTECTION OF STEEL WORKPIECES |
| US5260120A (en) * | 1991-12-06 | 1993-11-09 | Morton International, Inc. | Two coat weldable primer for steel |
| US20040018314A1 (en) * | 2002-07-25 | 2004-01-29 | Carrier Corporation | Primer adhesive for laminated condensing heat exchangers |
| US20040018313A1 (en) * | 2002-07-25 | 2004-01-29 | Carrier Corporation | Primer for painted metal used outdoors |
| CN101899257B (en) * | 2010-09-01 | 2012-07-11 | 北京虹霞正升涂料有限责任公司 | Heavy corrosion resistant, heat insulating and static conductive coating |
| EP3336366A1 (en) * | 2016-12-19 | 2018-06-20 | HILTI Aktiengesellschaft | Method for coating of a cold worked multi-cone anchoring element |
| EP3744796A1 (en) * | 2019-05-28 | 2020-12-02 | voestalpine Stahl GmbH | Coating system |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3437531A (en) * | 1962-07-26 | 1969-04-08 | Du Pont | Anhydrous chromic acid metal treating solution |
| US3382081A (en) * | 1965-09-02 | 1968-05-07 | Diamond Shamrock Corp | Chemical composition and method |
| GB1199657A (en) * | 1967-05-29 | 1970-07-22 | Diamond Shamrock Corp | Improvements in or relating to the Coating of Metal Surfaces |
| US3535167A (en) * | 1968-04-16 | 1970-10-20 | Diamond Shamrock Corp | Chromic acid-dimer acid coating composition for metals |
| US3519501A (en) * | 1968-04-16 | 1970-07-07 | Diamond Shamrock Corp | Chromic acid-organic coating compositions |
| US3535166A (en) * | 1968-04-16 | 1970-10-20 | Diamond Shamrock Corp | Chromic acid-organic dibasic acid coating compositions for metals |
| US3779794A (en) * | 1970-03-05 | 1973-12-18 | Essex Chemical Corp | Polyurethane sealant-primer system |
| US3679493A (en) * | 1970-03-11 | 1972-07-25 | Gaf Corp | Glycol ether-chromium corrosion resistant coatings for metallic surfaces |
| US3671331A (en) * | 1970-03-16 | 1972-06-20 | Diamond Shamrock Corp | Coated metal and method |
| US3687739A (en) * | 1970-12-10 | 1972-08-29 | Diamond Shamrock Corp | Coated metal and method |
| CA979337A (en) * | 1971-08-19 | 1975-12-09 | Irving Malkin | Coated metal and method |
| FR2193361A5 (en) * | 1972-07-19 | 1974-02-15 | Segard Norbert | Protective glossy coating for printed supports - from varnish contg nitro-cellulose surfacing resin with acrylic resin improving bond with support |
| SE387133B (en) * | 1972-10-18 | 1976-08-30 | Diamond Shamrock Corp | WAY TO PREPARE A BASIC TRANSFER COMPOSITION |
| SE387135B (en) * | 1972-10-18 | 1976-08-30 | Diamond Shamrock Corp | METHOD OF PREPARING A BASIC TRANSFER COMPOSITION AND FUNDS FOR IMPLEMENTING THE SET |
| US3990920A (en) * | 1974-05-06 | 1976-11-09 | Diamond Shamrock Corporation | Metal treating compositions of adjusted pH |
| US4020220A (en) * | 1975-03-20 | 1977-04-26 | Diamond Shamrock Corporation | Composite coating having enhanced corrosion resistance |
| CA1089155A (en) * | 1975-08-29 | 1980-11-11 | Wilbur S. Hall | Treating autodeposited coatings with cr composition |
-
1977
- 1977-06-20 US US05/807,785 patent/US4098620A/en not_active Expired - Lifetime
-
1978
- 1978-06-14 GB GB7826923A patent/GB2000050B/en not_active Expired
- 1978-06-19 MX MX173840A patent/MX148122A/en unknown
- 1978-06-19 DE DE2826827A patent/DE2826827C2/en not_active Expired
- 1978-06-19 FR FR7818217A patent/FR2395298A1/en active Granted
- 1978-06-19 SE SE7806986A patent/SE444001B/en not_active IP Right Cessation
- 1978-06-19 NL NLAANVRAGE7806602,A patent/NL182577C/en not_active IP Right Cessation
- 1978-06-19 BE BE188659A patent/BE868232A/en not_active IP Right Cessation
- 1978-06-19 JP JP53074065A patent/JPS593230B2/en not_active Expired
- 1978-06-19 ES ES470919A patent/ES470919A1/en not_active Expired
- 1978-06-19 IT IT49925/78A patent/IT1105548B/en active
- 1978-06-19 AU AU37225/78A patent/AU516375B2/en not_active Expired
- 1978-06-19 CA CA305,689A patent/CA1090662A/en not_active Expired
- 1978-06-20 BR BR787803900A patent/BR7803900A/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| NL182577C (en) | 1988-04-05 |
| SE7806986L (en) | 1978-12-21 |
| NL182577B (en) | 1987-11-02 |
| FR2395298A1 (en) | 1979-01-19 |
| DE2826827C2 (en) | 1983-12-01 |
| JPS593230B2 (en) | 1984-01-23 |
| AU516375B2 (en) | 1981-05-28 |
| AU3722578A (en) | 1980-01-03 |
| NL7806602A (en) | 1978-12-22 |
| US4098620A (en) | 1978-07-04 |
| JPS548636A (en) | 1979-01-23 |
| GB2000050A (en) | 1979-01-04 |
| DE2826827A1 (en) | 1979-01-04 |
| FR2395298B1 (en) | 1983-09-16 |
| GB2000050B (en) | 1982-01-13 |
| ES470919A1 (en) | 1979-10-01 |
| SE444001B (en) | 1986-03-17 |
| IT1105548B (en) | 1985-11-04 |
| BR7803900A (en) | 1979-01-16 |
| BE868232A (en) | 1978-12-19 |
| IT7849925A0 (en) | 1978-06-19 |
| MX148122A (en) | 1983-03-16 |
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